JASC 5531

Service difficulty reports · 1,234

Reports filed under 5531 · Vertical Stabilizer, Spar/Rib, newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE jasc_code = '5531'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR GLBA2012090400044Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB RT FWD SPAR CAP ANGLE AT 20 PERCENT CHORD AND APPROX VSS 84.10 PROTRUDING FROM THE 2ND FROM TOP FASTNER APPROX .125" TO EITHER SIDE, 2 CRACKS, .25" IN LENGTH. REPAIRED IAW EO 12-1900-5Sep 2, 2012 · N220GL · Beech 1900DSDR GLBA2012090400045Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACK IN THE VERTICAL STAB LT FWD SPAR CAP ANGLE AT 20 PERCENT CHORD AND APPROX VSS 84.10, EXTENDING FROM TOP OF ANGLE TO JUST PAST 2ND FROM TOP FASTENER, 1.5" IN LENGTH. REPAIRED IAW EO 12-1900-55-025.Aug 31, 2012 · N220GL · Beech 1900DSDR GLBA2012082100035Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND VERT STAB LT SPAR CAP ANGLE AT THE 20 PERCENT CHORD IS CRACKED AT THE UPPER END AT VSS 84.10, BEGINNING AT THE TOP EDGE AND RADIATES DOWNWARD, THE CRACK IS ON THE FWD FAIRING PORTION OF THE ANGLE, 4.25" IN LENGTH. Aug 20, 2012 · N154GL · Beech 1900DSDR ABXR2012080700057Rib · crackedVERTICAL L/E RIB AT FSS 417.69 ON VERTICAL STAB , CRACKED AT RT ATTACH POINT. REMOVED CRACKED RIB AND REPAIRED IAW SRM 55-30-09.Aug 7, 2012 · N365CM · Boeing 767328SDR GLBA2012080600027Spar Cap · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE LT VERTICAL STAB, LT FWD SPAR CAP ANGLE AT APPROX FSS 84.10, 20 PERCENT CHORD VISIBLE, 1.25" IN LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-55-021. MAJOR REPAIR.Aug 6, 2012 · N100UX · Beech 1900DSDR SWAA2012090407353Lug · corrodedVERTICAL STABILIZER AFT SPAR, LEFT PRIMARY ATTACH LUG, CORRODED AROUND AFT BUSHING FACE. REPAIRED LUG IAW EA.Jul 17, 2012 · N687SW · Boeing 7373Q8SDR SWAA2012090407352Lug · corrodedVERTICAL STABILIZER AFT SPAR, RT PRIMARY ATTACH LUG, CORRODED AROUND AFT BUSHING FACE. REPAIRED LUG IAW EA.Jul 17, 2012 · N687SW · Boeing 7373Q8SDR DALA1241839003Spar Cap · crackedVERTICAL STAB LEFT FRONT SPAR CAP CRACKED . COMPLIED WITH ERA 485915-14 AD REV A CODE 55-31.Jul 14, 2012 · N903DE · Doug MD88SDR DALA12005760918Spar · crackedCRACK ON VERTICAL STAB FRONT SPAR RT CHORD ZFS-53. ACCOMPLISHED ERA 477465-14 REV B CODE 9-55-31 REPAIRED.Jul 8, 2012 · N918DL · Doug MD88SDR FDEA201207032457Spar · crackedDURING HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION FOUND CRACK INDICATION AT LEFT NR 4 BANJO FITTING LOWER VERTICAL STAB FORWARD FLANGE OF UPPER REAR SPAR CAP. REPAIRED AS PER SRM 55-30-02 REPAIR 3 FIGURE 201 REVISION 49. REPAIR CLASSIFIED MAJOR AS PER GMMJul 3, 2012 · N613FE · Doug MD11FSDR FDEA201207032456Spar · crackedDURING HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION, FOUND CRACK INDICATION AT RT NR 4 BANJO FITTING LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP. REPAIRED AS PER SRM 53-30-02 FIGURE 201 REPAIR 3 REVISION 49 AND EA 1-5530-160973 PART 1. Jul 3, 2012 · N613FE · Doug MD11FSDR USAA2012062800014Attach Bolt · corrodedQ1 CHECK - RIGHT VERTICAL FIN FRONT SPAR ATTACH BOLT CORRODED AT BS 1016, S1R, BWL 300.50. REPLACED RIGHT VERTICAL FIN FRONT SPAR ATTACH BOLT IAW B737 AMM 55-30-00-004-001 & 55-30-00-404-017.Jun 12, 2012 · N433US · Boeing 7374B7SDR USAA2012062800013Attach Bolt · corrodedQ1 CHECK - LEFT VERTICAL FIN FRONT SPAR ATTACH BOLT CORRODED AT BS 1016, S1L, BWL 300.50. REPLACED LEFT VERTICAL FIN FRONT SPAR ATTACH BOLT IAW B737 AMM 55-30-00-004-001 & 55-30-00-404-017.Jun 12, 2012 · N433US · Boeing 7374B7SDR AALA20120608001Rib · damagedVERTICAL STABILIZER RIB THAT IS DIRECTLY ABOVE RUDDER IS DAMAGED. ACCOMPLISHED SPLICE REPAIR PER SRM 51-70-13-2R AND EA B737-55-024258.Jun 8, 2012 · N908AN · Boeing 737823SDR COEA2012060605917Stiffener · corrodedHEAVY CHECK / LEVEL 2 CORROSION: VERTICAL STAB FWD SPAR WEB STIFFENER APPROXIMATELY 5 INCHES ABOVE THE VOR ANTENNA HAS CORROSION (LENGTH .5", WIDTH 6", DEPTH .53"). REMOVED AND REPLACED STIFFENER WITH OEM PART PER ATR42 SRM.Jun 6, 2012 · N917FX · Aerosp ATR42300SDR COEA2012060604917Stiffener · corrodedHEAVY CHECK / LEVEL 2 CORROSION: VERTICAL STAB FWD SPAR WEB HAS CORROSION ON THE 2ND AND 3RD STIFFENERS FROM THE TOP (LENGTH .5", WIDTH 6", DEPTH .53"). REMOVED AND REPLACED STIFFENER WITH OEM PART PER ATR42 SRM.Jun 6, 2012 · N917FX · Aerosp ATR42300SDR COEA2012060603917Strap · corrodedHEAVY CHECK / LEVEL 2 CORROSION: VERTICAL STAB REAR SPAR WEB STRAP ABOVE PANEL 324AZ IS CORRODED (LENGTH 1", WIDTH 2", DEPTH .005"). REMOVED AND REPLACED WEB REAR SPAR STRAP WITH OEM PART PER ATR42 SRM.Jun 6, 2012 · N917FX · Aerosp ATR42300SDR AALA20120503003Spar Cap · damagedUNABLE TO PERFORM HFEC ROTARY HOLE PROBE INSPECTION TO AREA 12.5" BELOW LEFT SIDE OF VERTICAL STABILIZER FRONT SPAR CAP AT STATION ZFS=52.267, BECAUSE THE FASTENER HOLES IN THE SPAR CAP FORWARD FLANGE (12EACH) ARE OUT OF ALIGNMENT WITH REFERENCE TO HOLES IN THMay 3, 2012 · N565AA · Doug DC983SDR AALA20120424016Spar · damagedRIGHT VERTICAL STABILIZER, SEVENTH SPAR HOLE ABOVE STATION ZFS 52.267 OUT OF ROUND AND BEYOND LIMITS. INSTALLED DOUBLER TRIPLER PER EA MD80-55-023253 AND / SRM 51-30-10.Apr 24, 2012 · N595AA · Doug DC983SDR DALA1226689001Spar · crackedVERTICAL STABILIZER FRONT SPAR LT CHORD AT ZFS-52 CRACKED. ACCOMPLISH SECTION II REPAIR AT NEXT C-CHECK OR 3000 CYCLES AFTER SECTION 1, WHICHEVER COMES FIRST. REF NR 37 FOR FABRICATION OF SG09550005-3 REPAIR STRAP. 227037 REMOVED TEMPORARY REPAIR STRAP INSTAApr 24, 2012 · N901DE · Doug MD88SDR DALA1225149001Spar Cap · damagedDURING INSPECTION PER AD 2011-15-01 AND EA 09-470871-12AD, MTC NOTED 8 ELONGATED HOLES COMMON TO THE VERTICAL STABILIZER RT SPAR CAP LOCATED JUST ABOVE ZFS=52. THE SUBJECT CAP IS MACHINED TO VARYING THICKNESS OF 7075-T56 AL. REPAIR ACCOMPLISHED PER ER/A 5025Apr 19, 2012 · N901DE · Doug MD88SDR DALA1225139001Spar Cap · damagedDURING INSPECTION PER AD 2011-15-0, EA 09-470871-12, AND SECTION 111OF ER/A 488147-14AD REV B MTC NOTED 5 ELONGATED HOLES COMMON TO THE VERTICAL STABILIZER LT SPAR CAP LOCATED JUST ABOVE THE PREVIOUSLY BUSHED HOLE AT ZFS =52. THE SUBJECT CAP IS MACHINED TO VAApr 19, 2012 · N901DE · Doug MD88SDR DALA1225129001Spar · damagedWHILE IN MSP FOR PSV, AND DURING INSPECTION PER EA 09-470871-12AD, AN ELONGATED HOLE WAS FOUND ON THE LT LOWER AFT HOLE (HOLE COMMON TO LT SPAR FWD FLANGE). A BUSHING ONLY REPAIR FOR THIS HOLE LOCATION IS NOT ALLOWED PER SG09550004 REV "B". REPAIR ACCOMPLISApr 19, 2012 · N901DE · Doug MD88SDR DALA1220270997Spar · crackedVERTICAL STAB FRONT SPAR CAP HAS CRACK INDICATION IN FASTENER HOLE, LOWER LEFT AFT CORNER HOLE.Mar 29, 2012 · N997DL · Doug MD88SDR CHQA 20120318105Spar Cap · chafedDURING INSPECTION, THE VERTICAL FIN LEADING EDGE LEFT AND RIGHT FORWARD SPAR CAPS WAS FOUND THE BE CHAFED. THE VERTICAL FIN LEADING EDGE LEFT AND RIGHT FORWARD SPAR CAPS WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-004027.Mar 18, 2012 · N298SK · Emb EMB145LRSDR CHQA20120318104Spar Cap · chafedDURING INSPECTION, THE VERTICAL FIN LEADING EDGE LEFT AND RIGHT FORWARD SPAR CAPS WAS FOUND THE BE CHAFED. THE VERTICAL FIN LEADING EDGE LEFT AND RIGHT FORWARD SPAR CAPS WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-004027.Mar 18, 2012 · N298SK · Emb EMB145LRSDR IPXA2M72473Spar · damagedINSPECTION TYPE:2C, 2 SHEARED FASTENERS ON THE NR 4 BANJO FITTING TO PYLON CARRY-THROUGH CAP RT SIDE. REPAIRED THE VERTICAL STAB "BANJO FITTING" RT SIDE CARRY-THROUGH CAP IAW EO 5530-46430-A AND STA SA EA 011-5530-01-A3736 REV IR.Mar 8, 2012 · N278UP · Doug MD11FSDR FDEA201202220640Spar · crackedVERTICAL STABILIZER RT REAR CENTER SPAR TO REAR SPAR LOWER PANEL CRACKED. CARRIED OUT REPAIR IAW SRM 55-30-02 FIGURE 201 REVISION 48 AND SRM 51-33-01 REVISION 48. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 114.Feb 22, 2012 · N587FE · Doug MD11FSDR DALA1517959236Spar Cap · not reportedVERTICAL STABILIZER, L/E FRONT SPAR CAP REPAIRED IAW AA5530-01044.Jan 3, 2012 · N936DN · Doug MD9030SDR 29GA2011123195255Stringer · crackedDURING SCHEDULED C-6 INSPECTION DISCOVERED VERTICAL STABILIZER BAY 331 DL RIGHT OF CANTED RIB 54.026 ONE CRACK AT 39.5% CHORD STRINGER AND ONE CRACK AT VERTICAL STABILIZER BAY 331 CL RIGHT OF CANTED RIB 69.184 AT 49.25% CHORD STRINGER. INSTALLED REPAIRS AT RDec 31, 2011 · N47542 · Beech 1900DSDR DALA1503879235Spar Cap · unknownVERTICAL STABILIZER L/E FRONT SPAR CAP REPAIRED IAW AA 5530-01044.Dec 5, 2011 · N935DN · Doug MD9030SDR DALA1310720950Panel · damagedWHILE ACCOMPLISHING THE REPAIR TO THE SUBJECT VERTICAL STABILIZER IAW EA 09-470871-12 MAINT FOUND 3 HOLES ON THE LOWER LT AND 6 LOWER RT SIDE OF PANEL THAT WERE ALSO OVERSIZED. REPAIR ERA 498068-14.Nov 25, 2011 · N950DL · Doug MD88SDR FDEA201111235010Spar · misrepairedVERTICAL STABILIZER REAR SPAR MISREPAIRED. REPAIRED IAW EA1-5530-155843 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 113.Nov 23, 2011 · N624FE · Doug MD11FSDR FDEA201110144505Spar · chafedVERTICAL STAB RT MID SPAR CHORD IS CHAFED AT AFT END. REMOVED DAMAGED AREA IAW SRM 55-30-6 FIG 3. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLERS IAW SRM 55-30-6 FIG 3.Oct 14, 2011 · N213FE · Boeing 7272S2FSDR UALA2011101305561Rib · missingSPLICE ASSY AT UPPER END OF VERTICAL STABILIZER LEADING EDGE PANEL 321BL MISSING INTERNAL RIB.Oct 13, 2011 · N578UA · Boeing 757222SDR QMLD201110052601Rib · crackedTHE TOP RIB OF THE VERTICAL FIN WHERE THE ANTI COLLOSION LIGHT BASE IS MOUNTED, EXIBITS A CRACK RADIATING FROM THE NUTPLATE THAT IS MOUNTED UNDERNEATH.Oct 5, 2011 · N527MB · Bolkms BK117A4SDR FDEA201109073740Spar · crackedVERTICAL STABILIZER LEFT REAR CENTER SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED. REPAIRED AS PER SRM 55-30-02 REPAIR 2 FIG.201 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Sep 7, 2011 · N522FE · Doug MD11FSDR FDEA201109073739Spar · crackedVERTICAL STABILIZER RT REAR CENTER SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 55-30-02 FIG.201 REPAIR 2 REV 47. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 112.Sep 7, 2011 · N522FE · Doug MD11FSDR DALA1515039229Spar Cap · not reportedVERTICAL STABILIZER, L/E FRONT SPAR CAP REPAIRED IAW AA 5530-01044.Aug 16, 2011 · N929DN · Doug MD9030SDR IXXA20110812001Spar · corrodedDURING ROUTINE C-CHECK INSP FOUND RT VERTICAL STABILIZER REAR SPAR CORRODED AT STA ZR 45.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED STRAP AND FILLER. CLEANED, TREATED, PRIMED AREA Aug 12, 2011 · N41CX · Doug DC862FSDR DALA1145050949Spar · damagedDURING PSV VISIT IN MSP AN ELONGATED HOLE WAS FOUND ON THE LT SIDE OF THE VERTIAL STAB FRONT SPAR CHORD. THE SUBJECT HOLE WAS OPENED TO (0.218"). THE HOLE WAS OPENED IN THE SPAR CHORD TO ALLOW FOR 0.030" WALL MIN. ON REPAIR BUSHING. SEE FIG.1 DETAIL/LOCATIOJul 25, 2011 · N949DL · Doug MD88SDR DALA1145040949Spar · damagedDURING PSV VISIT IN MSP 6 DAMAGED HOLES WERE FOUND ON THE RT SIDE OF THE VERTICAL STAB FRONT SPAR CHORD. THE SUBJECT HOLES WERE OPENED TO NR 1-(0.218") NR 4-(0.218") NR 5-(0.218") NR -6(0.218") NR 7-(0.234") RESPECTIVELY. THE HOLES ARE OPENED IN THE SPAR CHOJul 25, 2011 · N949DL · Doug MD88SDR FDEA201106102197Spar · crackedVERTICAL STABILIZER REAR SPAR NR 4 BANJO FITTING SUSPECT CRACK AT STA 2164 AND ZID 54.5 AREA. (REFER TO SRM 55-30-02, FIG 201). REPAIRED AS PER SRM 55-30-02 FIG 201 REPAIR 3 REV 46. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 112. TO CARRY OUJun 10, 2011 · N645FE · Doug MD11FSDR DALA1139350989Spar · damagedDURING PSV IN MSP & INSP PER MD80-55A067/DAL EA 09-470871-12 ELONGATED HOLES WERE FOUND IN THE 5911394 LT SPAR CHORD, AT THE 12TH & 17TH HOLES ABOVE THE ZFS=52, SPLICE FIXED L/E TO REMOVABLE L/E SKIN SPLICE. THE HOLES WERE OPENED IN THE SPAR CHORD TO PROVIDE Jun 9, 2011 · N989DL · Doug MD88SDR FDEA201105282017Spar Cap · crackedCRACK INDICATION FOUND ON THE LOWER VERTICAL STABILIZER LEFT HAND UPPER FORWARD FLANGES OF THE REAR SPAR CAP. ACCOMPLISHED E.A.1-5530-149805, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.May 28, 2011 · N644FE · Doug MD11FSDR DALA1406009218Spar Cap · damagedVERTICAL STABILIZER, LEAD EDGE FRONT SPAR CAP DAMAGED. REPAIRED IAW AA 5530-01044.May 26, 2011 · N918DH · Doug MD9030SDR HYIA20110522002Rib · corrodedDURING HEAVY CHECK INSP FOUND VERTICAL STABILIZER LOWER RIB FLANGE IN CORRESPONDENCE TO THE 3 SPAR FITTINGS, WERE CORRODED BEYOND LIMITS. INSPECTION REF:ZL-324-GVI-10000/553601-DVI-10000 BEYOND LIMITS IAW SRM 57-36-00. DAMAGE WAS SUBMITTED THEN ISSUED S.R.I. DMay 22, 2011 · N42836 · Aerosp ATR42320SDR FDEA201105031705Spar Cap · crackedCRACK INDICATION FOUND ON THE LWR VERTICAL STAB ON THE RT UPPER FWD FLANGE OF THE REAR SPAR CAP FITTING. ACCOMPLISHED EA 1-5530-149805, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.May 3, 2011 · N644FE · Doug MD11FSDR CA110419013Spar · crackedLOWER FIN DEFECT WAS FOUND . THE TAILCONE WAS REMOVED TO INSPECT AND FOUND THE CRACK IN THE SPAR OF THE LOWER VERTICAL FIN.Apr 17, 2011 · Snias AS350BASDR GUUA94955040511BStringer · crackedDURING SCHEDULED ROUTINE INSP, DISCOVERED VERTICAL STAB RT SIDE APPEARS TO HAVE CRACKS AT EACH OF THE 3 CHORD STRINGERS AT CSS 54.026. STOP DRILLED CRACKS AND INSTALLED REPAIR STRAPS THREE EACH.Apr 5, 2011 · N69549 · Beech 1900D
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